Marcello Remedia
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Previous Organizations / Institutes
The organizations / institutes from the scholar's other articles in the past ten years
Research Subjects
Marcello Remedia has a total of 9 co-authors. Here are the top co-authors by number of shared publications:
- Guglielmo S. Aglietti
University of Auckland
6 shared publications Guy Richardson
3 shared publicationsAndrew Kiley
Airbus Defence and Space, Stevenage, England SG1 2AS, United Kingdom
2 shared publications- Charly A. Knight
University of Surrey
2 shared publications Matteo Appolloni
European Space Agency, 2201 AZ Noordwijk, The Netherlands
2 shared publicationsAlessandro Cozzani
1 shared publication
Latest Publications
- Open Access
- 1 May 2019
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 57 (5) , 2109-2122
Spacecraft Structure Model Validation and Test Philosophy
- 1 May 2019
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 57 (5) , 2109-2122
Open AccessSpacecraft Structure Model Validation and Test Philosophy
- 1 June 2018
- Published by Elsevier in Acta Astronautica
- Vol. 147, 205-218
Satellite Vibration Testing: Angle optimisation method to Reduce Overtesting
- 1 June 2018
- Published by Elsevier in Acta Astronautica
- Vol. 147, 205-218
Satellite Vibration Testing: Angle optimisation method to Reduce Overtesting
- 1 May 2015
- Published by Elsevier in Journal of Sound and Vibration
- Vol. 344, 138-157
A stochastic methodology for predictions of the environment created by multiple microvibration sources
- 1 May 2015
- Published by Elsevier in Journal of Sound and Vibration
- Vol. 344, 138-157
A stochastic methodology for predictions of the environment created by multiple microvibration sources
- 1 April 2015
- Published by Elsevier in Acta Astronautica
- Vol. 109, 88-102
Modelling the effect of electrical harness on microvibration response of structures
- 1 April 2015
- Published by Elsevier in Acta Astronautica
- Vol. 109, 88-102
Modelling the effect of electrical harness on microvibration response of structures
- 5 April 2013
- Published by American Institute of Aeronautics and Astronautics (AIAA)
A General Methodology for Analysis of Structure-Borne Micro-Vibration
Driven by the increasingly stringent stability requirement of some modern payloads (e.g. the new generations of optical instruments) the issue of accurate spacecraft micro-vibration modelling has grown of importance. This article focuses on the dynamic coupling between a source of micro-vibration (e.g. reaction wheel) and a structure, taking into account the uncertainties related to both parts. In this context, an alternative to the Monte Carlo Simulation for complex structures has been developed, consisting in sub-structural approach to perturb the natural frequencies of specific subsystem reduced with the Craig-Bampton method. In order to prove the validity of the method and its application to the theory of the coupling, benchmark examples and practical applications will be described. © 2013 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved
- 5 April 2013
- Published by American Institute of Aeronautics and Astronautics (AIAA)
A General Methodology for Analysis of Structure-Borne Micro-Vibration
Driven by the increasingly stringent stability requirement of some modern payloads (e.g. the new generations of optical instruments) the issue of accurate spacecraft micro-vibration modelling has grown of importance. This article focuses on the dynamic coupling between a source of micro-vibration (e.g. reaction wheel) and a structure, taking into account the uncertainties related to both parts. In this context, an alternative to the Monte Carlo Simulation for complex structures has been developed, consisting in sub-structural approach to perturb the natural frequencies of specific subsystem reduced with the Craig-Bampton method. In order to prove the validity of the method and its application to the theory of the coupling, benchmark examples and practical applications will be described. © 2013 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved